
High-Frequency Combustion Instabilities in Liquid Rocket Engines Driven by Propellants Flow Rate Oscillations
Author(s) -
Robin Nez,
Thomas Schmitt,
Sébastien Ducruix
Publication year - 2018
Publication title -
hal (le centre pour la communication scientifique directe)
Language(s) - English
Resource type - Conference proceedings
Subject(s) - liquid propellant rocket , propellant , aerospace engineering , combustion , rocket (weapon) , mechanics , flow (mathematics) , volumetric flow rate , control theory (sociology) , rocket propellant , rocket engine , materials science , physics , environmental science , aeronautics , engineering , computer science , chemistry , control (management) , organic chemistry , artificial intelligence